Using shock tube and coherent experimental technique, the sweeping process of shock wave in ground, forest belt and flame field is photographed, the sudden extinguish time of flame and the overpressure of shock wave w...Using shock tube and coherent experimental technique, the sweeping process of shock wave in ground, forest belt and flame field is photographed, the sudden extinguish time of flame and the overpressure of shock wave was measured. The research showed that it was obvious for shock wave extinguishing forest fire, the high dynamic pressure induced by shock wave may be the immediate cause of extinguishing flame. Moreover the overpressure, negative pressure and temperature rise of air causing by shock wave would make the combustible pyrolysis gas of forest tree mix with atmosphere then ignite and burn out, which probably is an important effect in restraining forest fire.展开更多
In a Mach 3.8 wind tunnel, both instantaneous and time-averaged flow structures of different scales around a blunt double-cone with or without supersonic film cooling were visualized via nano-tracer planar laser scatt...In a Mach 3.8 wind tunnel, both instantaneous and time-averaged flow structures of different scales around a blunt double-cone with or without supersonic film cooling were visualized via nano-tracer planar laser scattering （NPLS）, which has a high spatiotemporal resolution. Three experimental cases with different injection mass flux rates were carried out. Many typical flow structures were clearly shown, such as shock waves, expansion fans, shear layers, mixing layers, and turbulent boundary layers. The analysis of two NPLS images with an interval of 5 us revealed the temporal evolution characteristics of flow structures. With matched pressures, the laminar length of the mixing layer was longer than that in the case with a larger mass flux rate, but the full covered region was shorter. Structures like K-H （Kelvin-Helmholtz） vortices were clearly seen in both flows. Without injection, the flow was similar to the supersonic flow over a backward- facing step, and the structures were relatively simpler, and there was a longer laminar region. Large scale structures such as hairpin vortices were visualized. In addition, the results were compared in part with the schlieren images captured by others under similar conditions.展开更多
文摘Using shock tube and coherent experimental technique, the sweeping process of shock wave in ground, forest belt and flame field is photographed, the sudden extinguish time of flame and the overpressure of shock wave was measured. The research showed that it was obvious for shock wave extinguishing forest fire, the high dynamic pressure induced by shock wave may be the immediate cause of extinguishing flame. Moreover the overpressure, negative pressure and temperature rise of air causing by shock wave would make the combustible pyrolysis gas of forest tree mix with atmosphere then ignite and burn out, which probably is an important effect in restraining forest fire.
基金Project supported by the National Basic Research Program of China (Grant No. 2009 CB724100)the National Natural Science Foundation of China (Grant No. 11172326)
文摘In a Mach 3.8 wind tunnel, both instantaneous and time-averaged flow structures of different scales around a blunt double-cone with or without supersonic film cooling were visualized via nano-tracer planar laser scattering （NPLS）, which has a high spatiotemporal resolution. Three experimental cases with different injection mass flux rates were carried out. Many typical flow structures were clearly shown, such as shock waves, expansion fans, shear layers, mixing layers, and turbulent boundary layers. The analysis of two NPLS images with an interval of 5 us revealed the temporal evolution characteristics of flow structures. With matched pressures, the laminar length of the mixing layer was longer than that in the case with a larger mass flux rate, but the full covered region was shorter. Structures like K-H （Kelvin-Helmholtz） vortices were clearly seen in both flows. Without injection, the flow was similar to the supersonic flow over a backward- facing step, and the structures were relatively simpler, and there was a longer laminar region. Large scale structures such as hairpin vortices were visualized. In addition, the results were compared in part with the schlieren images captured by others under similar conditions.
